[IGSREPORT-22729] Wk 1790 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri May 16 11:37:42 PDT 2014
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1790 (Apr 27, 2014 - May 03, 2014)
Contacts: J. Griffiths (jake.griffiths at noaa.gov)
K. Choi (kevin.choi at noaa.gov)
COMBINATION STRATEGY:
---------------------
Starting with GPS week 860, the IGS Final orbit combination is done directly
in the ITRF without any alignment to the Bulletin B EOP series.
Each centre satellite clock corrections are first transformed to a common
reference. One of the following two methods can be used (the REMARKS section of
this report gives which method is used):
[1] For each centre, a clock offset and a drift are estimated with respect to
the broadcast clock corrections using only non-SA satellites;
[2] A chosen reference centre is aligned to the broadcast clock corrections
using all satellites. All other centres are then aligned to that reference
centre.
The offsets and drifts are used to align each centre satellite clock
corrections to GPS time. Ephemerides and clock corrections are then combined
as weighted averages computed over all centres. Each centre is given a
position weight and a clock weight. The position weights are computed from
each centre's absolute deviation to the unweighted average orbit after the
estimation of a 7-parameter Helmert transformation. The clock weights are
either computed from [1] the absolute deviation of the initial alignment to
broadcast clock for the non-SA satellites, or [2] from the absolute deviation
of centre's aligned clock corrections with respect to the unweighted mean.
Finally, a 7-parameter Helmert transformation and clock offset and drift are
estimated for each centre with respect to the combined solutions and parameters
and RMS of fit reported. All the above estimations are performed using the
L1-norm robust scheme.
Each centre ephemerides are also evaluated individually and independently from
the orbit combination by using week long arcs. The Earth Orientation Parameters
(EOP) used in this evaluation are those submitted by the respective centres.
The IGS combined orbits/clocks and all centres providing both orbit and clock
solutions are further evaluated by an independent point positioning (navigation)
program that uses both phase and pseudorange data at each SP3 epoch. This is
primarily intended for testing clock solution precision as well as the
orbit/clock consistency.
Like the clock solutions broadcast in the navigation message, the combined
satellite clocks are corrected for the periodical relativistic correction (see
e.g. GPS interface Control document ICD-GPS-200, p.73):
-2*(X.V)/c [distance unit],
where X and V are the inertial sv state and velocity vectors and c is the speed
of light. Also for compatibility with broadcast GPS time, the IGS clocks use
the linear combination of phase-smoothed P1 and P2 pseudorange data to remove
the 1st order ionospheric delay, with no other delay calibrations applied.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
PRODUCTS GENERATED:
-------------------
The resulting average ephemeris and clocks are output to daily files in SP3
format. The satellite accuracy codes displayed in the header are based on the
weighted RMS for each satellite over each daily arc. Note that each file
contains all the satellites that appear in any of the centre ephemeris files.
If a satellite or centre was excluded from combination, a note in the REMARKS
section of this report will identify the exclusion and the reason.
The resulting x and y earth rotation parameters (ERP) associated with the IGS
ephemeris files and their rates (xrt, yrt) are computed using a weighted average
of all available centres (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
Starting with GPS wk 0894, IGS LOD combinations were implemented in the
Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated
using Bulletin A most recent 10 days, i.e. up to 5 days prior to the last
non-predicted day of Bulletin A. AC LOD biases are removed and the new AC
bias-free LODs are used to compute a weighted IGS LOD which in turn is
integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as Bulletin
A fifth day prior to its last non-predicted day. Both IGS LOD and UT1-UTC
values are printed in the IGS Final erp file.
The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are:
igs1790[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1790[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1790[0-6].cls IGS GPS clock combination summary report.
igs17907.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17907.sum Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, EMR, ESA, GFZ, GRG, MIT, and
JPL. The other centres are excluded because of poorer consistency, they provide
broadcast clocks, or clock corrections are not provided (SIO). The clock
information not used is still compared to the combination for completeness. The
value of 999999.999999 microseconds, according to the SP3 format convention,
signifies that no clock solution is available and therefore must not be used.
In general, if an AC does not contribute to the terrestrial reference frame
(i.e. the SINEX combination), then any corresponding orbits & clocks
contributed from that AC should not be included with weight in this
combination. This is done to ensure a high level of consistency between the TRF
and the orbital frame. However, there is an exception for the clocks if the AC
is the reference center. In that case, only the clocks from that AC are
included with weight.
Starting week 1707:
cod = cof${wwww}[0-6].[clk,snx,sp3] & cod = cof${wwww}7.[erp,sum]
2. Rapid (IGR) orbits/clocks are included in the combination for statistics only.
Starting week 1582, a new orbit solution from CNES/GRGS (GRG) is included with
weight. GRG clocks are included with weight starting 12-Aug-2012 (GPS Week
1701, day 0, MJD 56151), after a procedural change to generate estimates in
the center-of-figure frame instead of the center-of-mass frame. GRG LOD
estimates are included for comparison only.
3. The following centre clock solutions, which provide broadcast clock
corrections, were excluded from the combination but kept in the combination
statistics:
-> Centre: NGS
4. The following clock solutions were excluded from the combination because they
were biasing the combined clock solutions (clock shifts/outliers) but were
kept for the RMS computation. Duplicate entries can arise due to separate
combination runs for the 30-s clocks ACs (listed first) and the 5-min clock
ACs (listed second).
Day | Centre | PRN/STA list
----+--------+---------------
0 | ESA | NTUS UNSA
0 | GFZ | 1 2 1 IRKJ NTUS HNLC IRKJ
0 | GRG | KOUC RBAY KOUC RBAY
0 | JPL | 32 POL2
0 | MIT | 25 25 IRKJ MDVJ PTBB FLIN IRKJ MDVJ PTBB
1 | COD | 25 25 NTUS INVK NTUS
1 | EMR | 25 25 MCM4 MCM4
1 | ESA | WUHN UNSA
1 | GFZ | 1 2 1 NTUS WUHN HNLC NTUS
1 | GRG | HYDE IRKJ MAL2 MONP HYDE MAL2
1 | JPL | 32 POVE
1 | MIT | 25 25 MDVJ
2 | COD | RBAY
2 | EMR | SFER SFER YAKT
2 | ESA | MBAR MONP UNSA
2 | GFZ | 1 2 1 RBAY REUN WUHN HNLC REUN WSRT WUHN
2 | GRG | CHUM GRAZ NICO RBAY REUN GRAZ NICO NTUS RBAY REUN
2 | MIT | 12 MDVJ GOPE MDVJ MOBS
3 | COD | MAC1 REUN
3 | EMR | CHUR SYOG CHUR SYOG WUHN
3 | ESA | ARTU KERG
3 | GFZ | 1 2 1 KERG NTUS HNLC KERG NTUS
3 | GRG | ARTU IRKJ MAC1 MAW1 REYK IRKJ MAC1 MAW1 WUHN
3 | JPL | CHUR WHIT
3 | MIT | 1 7 29 1 7 29 GOPE MAW1 MDVJ
4 | COD | 12
4 | EMR | WUHN WUHN
4 | ESA | NTUS MBAR NTUS
4 | GFZ | 1 2 1 25 ARTU GRAZ GRAZ HNLC NTUS
4 | GRG | REUN WUHN ARTU KELY NANO REUN SOFI WUHN
4 | MIT | FLIN MDVJ
5 | COD | BOR1 BOR1
5 | ESA | CHUR CHUR NKLG
5 | GFZ | 1 1 WUHN
5 | GRG | CHUR GRAZ RBAY WUHN CHUR GRAZ RBAY
5 | MIT | MDVJ GOPE MDVJ PDEL
6 | COD | 28 28
6 | EMR | WUHN
6 | ESA | UNSA
6 | GFZ | 1 2 1 WUHN HNLC WUHN
6 | GRG | RBAY HYDE NTUS RBAY
6 | MIT | 31 MDVJ GOPE MDVJ SCH2
5. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
6. The following orbit solutions were excluded from the combination because they
were biasing the weighted average (generally indicated by long arc RMS). They
were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
0 | GRG | 6
1 | GRG | 6
2 | GRG | 6
3 | GRG | 6
4 | GRG | 6
5 | GRG | 6
6 | GRG | 6
7. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
8. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | -.4 .5 -.8 -23 6 -6 .55
EMR | 0 | 5.2 -6.2 19.9 -10 5 -36 .47
ESA | 0 | .5 1.0 -1.3 -12 -5 22 .32
GFZ | 0 | .0 -.4 -1.9 -29 -46 1 .23
GRG | 0 | 4.2 -.8 13.3 13 26 -17 1.00
JPL | 0 | 7.0 -3.0 25.7 -84 -1 7 -.33
MIT | 0 | -2.3 .0 18.3 55 24 -9 .80
NGS | 0 | 2.6 -11.3 19.5 -107 -45 -26 .77
SIO | 0 | 3.1 4.4 14.9 18 -14 -6 .58
COD | 1 | -.7 .9 -1.8 -22 0 -8 .67
EMR | 1 | 2.9 -7.7 22.7 -17 -5 -39 .42
ESA | 1 | .8 -.1 -1.4 -6 -6 8 .43
GFZ | 1 | -.1 -.9 -2.6 -30 -33 -5 .34
GRG | 1 | 5.6 -3.4 15.9 14 18 0 .86
JPL | 1 | 2.0 -3.2 23.9 -31 -22 17 .17
MIT | 1 | -.9 -3.0 19.5 72 48 -55 .63
NGS | 1 | 1.3 -8.8 18.6 -90 -49 -25 .57
SIO | 1 | 6.4 1.5 19.1 -1 -7 8 .63
COD | 2 | -.2 .7 -.8 0 3 -23 .79
EMR | 2 | 5.8 -7.1 23.2 -14 6 -41 .92
ESA | 2 | .6 -.5 -.9 -6 -12 22 .58
GFZ | 2 | .2 -.3 -1.8 -10 -25 -18 .60
GRG | 2 | 2.5 -3.7 22.9 7 19 5 1.31
JPL | 2 | 2.6 -1.7 24.9 -31 58 44 .41
MIT | 2 | -.3 -.4 22.0 73 35 -22 .88
NGS | 2 | -3.0 -16.3 14.4 -113 10 -43 1.27
SIO | 2 | 4.3 3.2 16.7 -4 -14 13 .75
COD | 3 | -.4 .1 .3 -30 2 -57 .69
EMR | 3 | 1.1 -6.9 26.0 -25 4 -51 .92
ESA | 3 | .2 -.2 -.6 9 -32 33 .32
GFZ | 3 | .0 -.3 -1.6 -15 -42 -15 .10
GRG | 3 | .7 -7.0 15.1 -35 21 13 1.16
JPL | 3 | .0 -6.7 28.0 -69 61 11 -.18
MIT | 3 | -.3 -5.3 20.2 2 11 21 .78
NGS | 3 | .8 -12.8 22.9 -119 -50 -35 .63
SIO | 3 | -3.7 .2 5.3 -31 -20 -6 .56
COD | 4 | -.5 .2 -.9 -50 0 -67 .36
EMR | 4 | 9.0 -1.3 19.0 -17 14 -65 .76
ESA | 4 | 1.4 .4 -1.0 18 1 5 .46
GFZ | 4 | .1 .5 -.7 -43 -37 -20 .18
GRG | 4 | 1.7 -3.7 19.9 -27 25 -26 .96
JPL | 4 | -2.3 -2.9 21.7 -75 -27 17 .45
MIT | 4 | -.5 -3.4 23.2 7 16 -60 .67
NGS | 4 | -1.8 -.7 32.4 -95 -57 -11 .55
SIO | 4 | -2.7 -.6 .6 -16 -17 -17 .47
COD | 5 | -.9 1.0 -1.0 -51 -3 -40 .54
EMR | 5 | .2 -3.0 8.6 -5 3 -41 .77
ESA | 5 | .6 1.0 -1.0 5 -20 16 .41
GFZ | 5 | .3 .4 -.7 -41 -23 -28 .08
GRG | 5 | -.1 1.2 22.9 -4 25 -22 .76
JPL | 5 | -2.9 -1.4 17.6 -48 35 0 -.37
MIT | 5 | -.4 .4 22.2 30 -18 67 .47
NGS | 5 | -3.3 3.1 15.3 -35 6 -13 .51
SIO | 5 | 1.1 3.2 -2.6 -25 -8 -24 .38
COD | 6 | -1.2 1.2 -.7 -24 4 -57 .49
EMR | 6 | 3.3 -1.8 12.1 -10 4 -41 .50
ESA | 6 | .5 .3 -1.2 -13 2 -2 .24
GFZ | 6 | .0 .0 -1.1 -28 -26 -31 -.03
GRG | 6 | 3.7 -1.6 20.4 -33 19 -28 .72
JPL | 6 | -1.4 -3.9 16.1 -68 37 11 -.29
MIT | 6 | 4.4 -1.2 17.5 12 -3 -18 .50
NGS | 6 | -.1 -4.0 21.2 -73 2 -13 .58
SIO | 6 | 1.1 3.0 -14.6 -32 -32 -18 .35
9. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
10. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (Table 1.1790.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1790.b).
The second part, Table 2, contains the complete ephemeris and clock
correction transformation parameters (includes both the apriori and a
posteriori values) for each centre and each day (Tables 2.1790.[0-6]).
The third part, Table 3, contains two types of daily RMS for each satellite
and centre, along with the computed satellite position sigmas for the
combined orbits (Tables 3.1790.[0-6]). The first type of satellite RMS is
based on orbit combination and the second RMS type is a result of the 7-day
arc evaluation of each centre ephemerides. The fourth part, Table 4, is a
weekly summary of the daily precise navigation summaries for centres
providing both orbit and clock solutions. It contains weekly station RMS
w.r.t. the initial coordinates for the Latitude, Longitude and Height
components for up to three IGS stations (Table 4.1307). The fifth part,
Table 5, is similar to Table 4 and contains daily precise navigation
statistics (Tables 5.1790.0-6). The sixth part, Table 6, is a weekly
summary of daily ERP combination statistics. The seventh part, Table 7,
contains the daily ERP statistics. But this is not the IGS official ERP
combination products (which come from the accompanying SINEX combination)
but provided to check combination consistency, etc.
In Tables 1-3, the most important statistic which is meaningful for intra
centre/satellite analysis is labeled WRMS. It is a weighted RMS where
normalized weights are based on accuracy codes given in the SP3 files, and
should not be affected by downweighted/problem satellites when acknowledged
by individual centres in their SP3 file.
Table 1: Week 1790 summary. (Apr 27, 2014 - May 03, 2014)
Table 1.1790.a GPS week: 1790 MJD: 56774.000-56780.000
Mean and standard deviations of transformation parameters to the
combined IGS orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 246| 0 0 -2 5 23 -10 -.01 10 9 | -933 -215 17 109
| 0 0 2 21 26 5 .04 | 505 859
emr 80| 0 -1 3 18 -34 44 .22 13 13 | 3310 -377 15 139
| 1 1 1 23 12 17 .03 | 1433 1103
esa 150| 0 0 -4 2 2 -11 -.38 12 12 | -504 -328 10 154
| 0 0 1 19 8 8 .02 | 802 1628
gfz 196| 0 0 -4 0 4 0 .06 12 12 | 67 -233 12 134
| 0 1 1 17 23 7 .03 | 335 637
grg 183| 2 0 9 -17 -18 6 .26 16 15 | -38 -153 16 165
| 1 1 3 11 16 8 .03 | 215 437
igr n/a| 0 0 -3 -3 18 -13 -.22 5 5 | 9058 -114 16 85
| 0 0 0 24 14 10 .04 | 809 991
jpl 80| 0 1 -3 -19 9 10 -.01 13 12 | 3092 -489 16 151
| 1 1 1 10 16 23 .03 | 1473 1055
mit 299| 0 -1 6 44 1 2 -.06 13 11 | -27 -352 24 211
| 1 1 1 38 27 45 .02 | 170 404
ngs 228| 0 0 0 -46 -3 -29 .01 12 10 | -968 -156 1774 3271
| 0 1 1 77 45 18 .07 | 450 743
sio 488| -1 2 -10 -15 -17 -19 -.70 22 21 | --- --- --- ---
| 0 1 2 18 23 23 .09 | --- ---
Table 1.1790.b GPS week : 1790 MJD: 56774.000-56780.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 4 5 5 4 4 4 |
2 | 5 4 4 4 4 4 4 |
3 | 4 4 4 4 4 4 4 |
4 | 4 5 4 4 4 4 4 |
5 | 6 6 6 6 6 5 5 |
6 | 0 0 0 0 0 0 0 |
7 | 5 5 5 6 5 5 5 |
8 | 4 4 4 4 4 4 4 |
9 | 4 4 4 4 4 4 6 |
10 | 5 4 4 5 4 4 4 |
11 | 5 5 5 5 4 5 5 |
12 | 5 5 5 5 5 5 6 |
13 | 5 5 5 6 5 5 5 |
14 | 5 5 5 5 4 4 4 |
15 | 5 5 5 5 5 5 5 |
16 | 5 5 5 5 5 5 6 |
17 | 6 5 6 5 5 5 6 |
18 | 5 5 5 5 4 4 5 |
19 | 5 5 5 5 5 5 5 |
20 | 4 4 4 5 4 5 5 |
21 | 4 4 4 5 4 5 4 |
22 | 4 4 5 4 4 4 4 |
23 | 5 5 5 6 5 5 5 |
24 | 5 4 4 4 4 4 4 |
25 | 5 6 6 6 6 5 5 |
26 | 5 4 4 4 4 4 4 |
27 | 5 5 5 5 5 5 5 |
28 | 4 4 4 4 4 4 4 |
29 | 6 5 6 6 5 5 6 |
30 | 0 0 0 0 0 0 0 |
31 | 6 6 6 6 5 5 6 |
32 | 6 6 6 6 6 5 5 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1790.0 GPS week: 1790 Day: 0 MJD: 56774.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 254| 0 0 0 14 8 -5 .01 10 10 | -1532 896 17 104
emr 80| 0 -4 4 32 -31 74 .17 13 13 | 3724 892 15 136
esa 150| 1 1 -3 -5 1 -5 -.38 13 13 | -224 -1372 10 142
gfz 197| 0 -1 -4 14 8 0 .03 12 11 | 78 -404 15 133
grg 188| 3 1 3 -3 -17 -8 .27 14 14 | -369 343 15 163
igr n/a| 0 0 -3 -9 21 -14 -.22 6 5 | 8765 1002 17 75
jpl 80| -2 1 -3 -21 -7 25 -.05 12 12 | 3692 761 16 148
mit 299| -1 0 4 63 -3 9 -.08 14 11 | -125 -361 25 200
ngs 230| 0 -1 0 -84 32 -68 .03 12 10 | -1379 675 1801 3148
sio 511| 0 3 -10 0 -45 -45 -.71 20 18 | --- --- --- ---
Table 2.1790.1 GPS week: 1790 Day: 1 MJD: 56775.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 252| 1 1 0 43 7 -20 .02 9 9 | -902 -447 19 108
emr 80| 0 -4 3 38 -47 58 .20 14 14 | 5300 -673 14 141
esa 150| 0 0 -4 0 -2 -13 -.37 13 13 | 396 -2864 11 164
gfz 196| 0 -1 -5 -7 -13 3 .06 11 10 | -18 390 11 130
grg 187| 3 0 12 -8 -43 6 .28 16 15 | 77 -95 16 152
igr n/a| 0 1 -5 -39 11 -7 -.25 5 5 | 10469 -757 16 86
jpl 80| 0 0 -5 -18 15 53 -.03 13 12 | 5161 -992 17 171
mit 299| -2 -2 4 97 41 -46 -.07 11 10 | 77 -343 25 204
ngs 230| 0 0 0 -166 22 -25 -.00 12 10 | -948 -357 2132 3623
sio 500| -1 2 -11 2 -7 -4 -.76 22 21 | --- --- --- ---
Table 2.1790.2 GPS week: 1790 Day: 2 MJD: 56776.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 247| 1 0 -1 -9 -5 -15 -.06 9 9 | -1165 30 16 109
emr 80| 3 0 4 -10 -22 42 .25 13 13 | 3795 617 17 154
esa 150| 0 1 -3 -14 -7 3 -.39 13 13 | -2010 1706 10 153
gfz 198| 0 0 -5 -18 22 2 .07 12 11 | -266 68 11 130
grg 183| 0 0 11 -13 6 18 .29 15 15 | -315 337 16 157
igr n/a| 0 0 -3 -13 16 -22 -.26 5 5 | 8775 974 16 86
jpl 80| -1 2 -4 -13 23 7 -.01 13 12 | 3418 691 18 143
mit 300| 0 -1 6 79 23 -33 -.06 12 10 | -355 262 27 208
ngs 226| -1 -2 -2 -29 -41 -23 .15 14 12 | -1394 346 1253 3097
sio 488| -1 4 -12 -7 -12 -31 -.80 21 21 | --- --- --- ---
Table 2.1790.3 GPS week: 1790 Day: 3 MJD: 56777.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 240| 0 1 0 -20 64 -11 -.07 12 12 | -1056 -299 21 132
emr 80| 0 -1 2 -18 -25 25 .22 13 13 | 4147 -949 18 159
esa 150| 0 0 -5 -24 18 -5 -.37 13 13 | -634 1214 11 159
gfz 195| 0 0 -6 5 27 2 .09 11 11 | -305 90 12 158
grg 180| 3 -1 9 -38 -11 7 .23 16 17 | -7 -217 17 190
igr n/a| 0 0 -4 26 37 -31 -.22 6 6 | 9501 -450 18 95
jpl 80| 0 5 -4 -35 31 -7 .00 15 15 | 3892 -863 19 167
mit 299| 0 -3 5 29 -7 5 -.07 12 10 | -45 -138 20 232
ngs 226| -1 -1 1 61 -88 -24 .04 12 10 | -1057 -305 1619 3353
sio 475| -1 1 -10 -27 -34 -38 -.73 22 24 | --- --- --- ---
Table 2.1790.4 GPS week: 1790 Day: 4 MJD: 56778.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 238| 0 1 -4 -9 27 -3 -.03 8 8 | -1136 270 16 100
emr 80| 1 -1 1 28 -28 37 .23 13 13 | 3088 -977 16 130
esa 150| -1 0 -4 9 5 -20 -.39 13 13 | 221 -268 11 153
gfz 196| 0 0 -3 -14 -17 8 .07 13 12 | -13 369 11 136
grg 182| 2 1 9 -16 -38 6 .20 15 14 | 45 -20 17 186
igr n/a| 0 0 -2 -20 36 0 -.23 5 5 | 9197 -354 17 88
jpl 80| 2 0 -3 -22 -12 11 .03 13 13 | 2865 -776 16 149
mit 300| 0 -2 6 -19 12 -13 -.07 11 10 | 44 -257 24 191
ngs 230| 0 0 3 33 27 -24 .00 11 10 | -1116 240 1546 3328
sio 480| -1 2 -10 -48 -26 -26 -.63 22 20 | --- --- --- ---
Table 2.1790.5 GPS week: 1790 Day: 5 MJD: 56779.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 243| 0 0 -3 5 55 -10 .03 8 8 | -839 -66 20 113
emr 80| -1 0 3 37 -55 39 .24 13 13 | 2295 -2119 15 131
esa 150| 0 0 -4 27 -4 -21 -.36 12 12 | -894 607 11 157
gfz 197| 0 0 -2 -13 -23 -12 .02 13 12 | 638 -914 13 122
grg 183| 2 -1 9 -12 -15 6 .25 15 15 | 142 -627 16 154
igr n/a| 0 0 -2 27 10 -8 -.13 5 5 | 8875 -1702 18 72
jpl 80| 1 0 -2 0 -2 -20 -.01 12 12 | 2098 -2231 16 148
mit 300| 2 -2 7 35 -11 93 -.05 13 12 | 51 -570 23 226
ngs 229| 0 0 0 -82 3 -31 -.02 11 10 | -820 -74 2325 3357
sio 481| 0 1 -6 -22 27 -10 -.54 23 21 | --- --- --- ---
Table 2.1790.6 GPS week: 1790 Day: 6 MJD: 56780.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 248| 0 0 -5 9 6 -8 .01 9 9 | 94 -1894 16 99
emr 80| 0 0 2 21 -29 29 .24 11 11 | 825 569 15 123
esa 150| 0 0 -2 25 6 -13 -.41 11 11 | -384 -1323 10 151
gfz 199| -1 1 -3 28 31 -7 .05 14 13 | 360 -1232 14 130
grg 182| 2 -1 14 -28 -11 11 .30 17 16 | 158 -795 19 153
igr n/a| 0 0 -3 2 -4 -11 -.23 5 5 | 7824 487 16 94
jpl 80| 0 1 -2 -22 17 3 .02 12 11 | 524 -19 16 136
mit 299| 2 -1 6 27 -45 6 -.04 17 14 | 158 -1059 26 222
ngs 227| -1 0 1 -61 19 -7 -.10 11 10 | -66 -1622 1744 2995
sio 482| -1 2 -9 -7 -25 22 -.74 23 22 | --- --- --- ---
Table 3: Daily fit for each satellite and each centre resulting from weighted
average combination and from long arc orbit dynamics (7-day). The
first IGS column gives resulting satellite accuracy measures found in
SP3 header. The last IGS column gives the RMS fit of the IGS orbit
when processed through the 7-day arc evaluation.
"E" stands for eclipsing satellites (earth).
"M" stands for eclipsing satellites (moon).
"X" stands for excluded from the statistics but included in IGS orbit.
"T" stands for Total long arc orbit RMS for all satellites.
"NE" stands for long arc orbit RMS for Non-Eclipsing satellites only.
"MEDI" stands for median of the centre's satellite RMS.
"MD"
Units: mm.
Table 3.1790.0 GPS week: 1790 Day: 0 MJD: 56774.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 9 8 13 12 11 6 12 11 11 12 4 | 34 39 32 38 38 33 41 34 34 31 34
2 | 10 14 12 15 11 6 12 12 10 33 4 | 18 29 23 22 22 17 24 21 24 21 19
3 | 9 7 13 11 11 4 7 9 9 45 3 | 32 35 31 32 31 31 32 29 34 48 30
4 | 7 8 12 10 9 5 9 14 11 11 4 | 26 28 24 28 29 23 26 28 28 25 25
5 | 12 22 6 15 18 5 21 15 13 17 6 | 18 30 16 24 30 19 29 23 28 24 20
X6E | 1 --- --- --- 299 113 --- --- --- --- 0 | 81 --- --- --- 134 84 --- --- --- --- 80
7 | 8 11 18 12 13 4 11 12 11 22 4 | 32 37 28 36 37 29 32 29 30 33 30
8 | 5 9 14 12 14 4 10 14 9 14 4 | 23 28 22 25 20 20 25 22 25 21 22
9 | 6 12 14 11 12 4 8 10 10 13 4 | 38 42 36 41 35 36 40 37 39 35 37
10 | 18 15 15 13 13 10 13 9 9 21 5 | 53 60 55 56 59 54 58 51 55 62 54
11 | 9 9 16 12 13 4 9 11 13 22 4 | 33 40 27 36 45 31 37 39 32 34 34
12E | 9 13 8 12 22 5 17 14 9 9 5 | 47 50 46 52 45 44 47 48 46 45 46
13 | 7 16 14 11 20 5 12 13 12 13 5 | 34 32 29 42 42 32 36 37 35 32 33
14 | 9 17 12 14 16 9 11 16 8 16 5 | 33 30 27 40 36 31 32 31 30 29 30
15 | 12 18 12 12 18 5 15 15 11 20 5 | 26 31 18 32 32 23 26 27 30 29 24
16E | 11 15 13 8 18 6 12 15 13 18 5 | 47 45 42 45 42 43 42 46 45 38 43
17 | 12 20 15 15 13 5 14 18 13 25 5 | 31 38 29 37 38 29 31 44 38 33 32
18 | 10 11 9 10 16 6 14 12 13 15 4 | 31 29 32 27 28 31 37 25 31 32 28
19 | 8 10 13 14 15 4 12 15 11 20 4 | 30 34 26 32 34 28 29 37 26 25 28
20 | 7 10 9 10 14 6 8 9 10 25 3 | 30 31 32 31 27 27 31 25 30 37 28
21 | 12 11 13 9 13 4 11 11 11 22 4 | 20 25 24 22 21 20 26 24 25 20 20
22 | 8 12 11 9 12 4 9 12 12 15 4 | 31 32 31 31 32 29 35 27 32 30 29
23 | 8 14 13 14 13 3 13 10 9 23 4 | 26 33 24 37 33 27 28 29 31 28 28
24 | 9 9 15 10 16 3 14 14 8 12 4 | 25 28 25 28 30 22 28 24 25 22 24
25E | 13 13 16 12 10 5 12 16 14 10 5 | 85 84 84 86 83 83 123 86 87 86 84
26 | 10 12 13 11 11 6 8 19 14 20 4 | 25 24 21 27 23 22 26 29 27 30 23
X27 | 16 10 18 10 --- 5 11 11 13 12 5 | 33 28 21 28 --- 23 29 30 24 19 26
28E | 7 10 11 10 14 4 12 9 9 16 4 | 36 36 32 35 39 32 35 36 36 34 34
29 | 12 16 15 13 13 5 16 16 12 25 5 | 26 29 26 27 27 22 28 25 25 27 23
X30 | 1 --- --- --- --- 16 --- --- --- --- 0 | 47 --- --- --- --- 42 --- --- --- --- 47
31 | 15 13 14 12 19 7 10 24 14 19 5 | 27 34 23 32 37 23 29 26 29 22 25
32E | 9 17 11 11 14 10 14 16 25 19 5 | 116 119 111 113 115 115 116 118 117 113 114
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 13 12 14 6 12 14 12 20 |T 37 38 33 38 41 35 38 36 36 35 36
WRMS | 10 13 13 11 14 5 12 11 10 18 |NE 29 32 26 31 32 27 31 29 30 30 27
MEDI | 9 12 13 12 13 5 12 13 11 18 |MD 31 32 27 32 34 29 31 29 30 30 29
Table 3.1790.1 GPS week: 1790 Day: 1 MJD: 56775.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 7 14 7 17 5 13 7 9 24 4 | 27 33 25 30 34 24 33 27 25 25 27
2 | 12 12 13 10 12 6 11 10 9 30 4 | 18 24 21 17 21 15 20 17 15 13 16
3 | 5 10 14 11 15 4 10 7 12 45 4 | 30 32 28 30 32 26 28 28 29 47 28
4 | 15 12 14 9 13 6 7 13 15 17 4 | 33 27 26 26 29 21 24 27 23 24 25
5 | 9 24 8 15 18 3 19 14 10 17 5 | 22 30 16 22 28 17 26 20 19 21 18
X6E | 3 --- --- --- 551 85 --- --- --- --- 0 | 98 --- --- --- 177 123 --- --- --- --- 96
7 | 10 13 16 12 15 4 11 13 11 23 4 | 33 35 29 34 35 26 29 32 30 33 30
8 | 7 11 14 11 15 4 10 8 12 22 4 | 22 28 23 24 23 19 22 23 22 29 22
9 | 6 12 14 11 14 3 11 6 11 26 4 | 40 43 40 40 40 38 39 42 40 46 39
10 | 8 13 14 10 17 10 13 8 8 21 4 | 27 29 26 27 28 23 28 27 23 31 25
11 | 8 10 16 8 18 5 12 9 12 22 4 | 29 38 24 30 41 23 31 30 28 30 29
12E | 8 14 10 9 25 5 19 10 9 8 5 | 36 38 32 36 37 32 32 33 35 31 33
13 | 7 14 17 15 17 4 13 12 11 15 5 | 25 31 23 30 35 24 26 27 24 26 25
14 | 8 15 11 10 14 7 12 13 18 16 4 | 31 29 26 34 31 26 27 28 33 26 28
15 | 11 19 10 13 13 4 14 12 13 14 5 | 26 34 22 29 29 22 26 28 27 24 25
16E | 9 19 13 10 17 6 15 10 12 17 5 | 38 39 34 39 38 35 35 40 40 37 36
17 | 11 15 15 11 15 7 15 17 12 24 5 | 24 33 26 26 33 24 29 35 27 26 26
18 | 10 13 9 10 15 6 16 10 11 16 4 | 27 24 24 22 25 21 27 21 17 27 21
19 | 6 13 14 12 20 3 12 10 12 22 4 | 27 33 26 30 34 24 28 30 28 20 27
20 | 7 11 9 10 19 5 10 9 9 22 4 | 25 27 23 26 25 22 23 20 23 30 22
21 | 10 9 13 8 13 5 12 9 8 22 4 | 19 21 19 15 18 12 18 18 14 15 14
22 | 10 10 9 8 17 4 10 9 7 14 4 | 25 23 20 20 23 18 21 20 18 24 18
23 | 7 18 11 19 13 5 16 10 9 25 5 | 26 34 24 34 32 24 24 26 25 27 25
24M | 9 13 14 7 17 4 13 9 10 10 4 | 31 37 31 29 32 26 33 28 28 28 29
X25E | 12 18 14 11 15 7 --- 16 18 11 6 | 113 112 112 111 113 113 --- 115 121 111 113
26 | 8 11 12 7 14 5 10 11 8 24 3 | 24 26 22 24 24 20 23 27 21 30 23
X27 | 7 7 14 15 --- 5 12 10 14 10 4 | 24 27 22 27 --- 21 28 26 25 17 24
28E | 8 14 10 10 15 4 11 6 11 10 4 | 34 36 30 34 44 30 32 33 31 30 32
29M | 9 18 13 11 12 7 19 15 14 26 5 | 30 31 30 30 27 26 31 27 30 36 27
X30 | 3 --- --- --- --- 23 --- --- --- --- 0 | 40 --- --- --- --- 35 --- --- --- --- 39
31 | 10 17 13 13 16 5 13 22 14 21 5 | 25 38 23 32 35 22 30 25 26 20 25
32E | 14 20 12 14 16 7 14 18 23 22 6 | 142 145 138 134 139 137 141 141 135 140 139
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 14 13 11 16 5 13 11 12 22 |T 36 37 32 34 42 33 31 34 32 34 34
WRMS | 9 14 13 10 15 5 12 10 10 21 |NE 25 29 23 26 28 21 26 24 23 25 23
MEDI | 8 13 13 10 15 5 12 10 11 21 |MD 27 32 25 30 32 24 28 27 26 27 26
Table 3.1790.2 GPS week: 1790 Day: 2 MJD: 56776.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 10 6 14 11 17 6 12 7 17 12 4 | 26 32 28 33 35 28 36 31 33 28 29
2 | 10 11 13 10 11 4 12 8 12 30 4 | 14 25 20 16 19 12 21 18 18 10 15
3 | 7 8 13 13 12 3 8 9 12 38 4 | 23 25 22 23 24 19 25 20 24 39 21
4M | 9 9 11 8 14 6 11 11 12 15 4 | 26 31 25 26 30 23 27 28 30 24 26
5 | 11 19 7 13 19 4 20 14 12 22 5 | 24 28 16 20 27 17 26 18 23 24 18
X6E | 2 --- --- --- 559 87 --- --- --- --- 0 | 75 --- --- --- 154 87 --- --- --- --- 75
7M | 10 11 14 15 14 3 12 9 15 24 4 | 35 39 31 43 40 33 37 35 36 36 35
8 | 7 10 14 12 13 5 9 5 11 20 4 | 16 24 16 16 17 14 20 16 24 22 16
9M | 7 12 14 10 13 6 10 12 10 26 4 | 28 35 29 29 33 28 29 27 33 37 29
10 | 7 13 13 11 11 7 11 8 8 17 4 | 28 30 30 29 26 27 31 28 31 31 27
11 | 9 9 16 11 17 5 10 11 17 30 4 | 24 34 24 28 41 25 32 33 26 38 27
12E | 10 17 8 11 17 4 19 9 17 9 5 | 44 45 39 41 56 39 39 39 47 34 42
13M | 9 14 14 11 20 4 12 13 10 13 5 | 28 32 25 33 40 27 31 33 33 29 29
14 | 9 18 12 16 14 9 15 9 7 19 5 | 28 29 27 36 33 27 31 30 37 27 29
15 | 10 19 12 10 14 4 15 9 15 17 5 | 25 32 17 24 29 18 24 25 27 19 22
16E | 10 21 9 14 13 5 14 9 14 14 5 | 35 32 33 42 38 33 34 35 38 26 34
17M | 11 14 15 12 18 6 16 20 17 24 5 | 23 31 29 28 34 25 30 38 34 31 27
18 | 9 11 11 12 17 3 14 10 12 17 4 | 23 25 24 20 29 20 26 16 21 24 20
19 | 7 11 13 16 16 5 12 12 14 24 4 | 26 31 26 32 32 27 31 32 26 26 27
20 | 9 10 10 9 14 6 10 9 16 21 4 | 27 28 30 30 28 27 28 25 39 30 27
21 | 9 10 15 10 12 4 11 10 11 25 4 | 14 23 19 16 22 13 21 17 17 16 15
22M | 7 14 11 11 17 8 9 20 12 16 5 | 26 26 25 21 26 22 27 31 29 27 24
23M | 8 15 12 12 17 4 13 8 9 22 4 | 25 30 22 34 36 23 26 26 35 24 27
24M | 6 9 15 8 10 5 11 7 13 19 3 | 25 28 24 25 29 21 25 22 26 23 24
X25E | 14 17 15 10 13 6 --- 17 19 18 6 | 72 78 73 68 81 70 --- 67 69 63 71
26 | 10 11 11 8 13 7 9 9 13 28 4 | 21 23 19 21 21 17 20 20 19 31 18
X27 | 10 9 14 14 --- 5 13 8 15 13 5 | 26 25 23 23 --- 21 32 25 26 19 24
28E | 8 14 8 9 19 4 13 7 13 19 4 | 36 37 33 35 40 32 34 35 39 36 34
29 | 12 16 14 13 13 6 17 15 17 24 5 | 31 36 30 28 30 25 33 24 28 28 27
X30M | 2 --- --- --- --- 22 --- --- --- --- 0 | 32 --- --- --- --- 33 --- --- --- --- 32
31 | 18 14 14 14 16 7 13 21 13 17 6 | 31 36 23 35 36 24 31 24 30 21 26
32E | 8 16 14 14 16 7 14 16 21 15 5 | 89 92 86 87 86 86 86 83 83 85 86
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 13 12 15 5 13 12 14 21 |T 31 34 28 31 39 29 30 30 32 30 30
WRMS | 9 13 13 11 15 5 12 10 12 21 |NE 23 28 22 25 27 21 27 23 26 25 22
MEDI | 9 12 13 11 14 5 12 9 13 19 |MD 26 31 25 28 32 25 30 27 30 27 27
Table 3.1790.3 GPS week: 1790 Day: 3 MJD: 56777.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 11 8 14 13 17 6 16 10 11 9 4 | 33 41 31 40 39 32 41 36 37 32 35
2 | 10 10 12 11 9 7 14 9 10 35 4 | 21 28 25 25 23 22 25 24 28 23 23
3 | 10 8 11 11 16 4 8 8 14 44 4 | 31 32 28 30 32 29 30 30 39 49 30
4 | 10 10 9 8 13 8 11 11 10 16 4 | 32 30 27 30 28 25 30 29 29 28 28
5 | 9 19 7 15 19 6 22 13 8 23 5 | 28 34 26 31 34 24 35 26 31 29 28
X6E | 4 --- --- --- 325 119 --- --- --- --- 0 | 91 --- --- --- 204 99 --- --- --- --- 89
7 | 13 13 15 15 16 6 14 17 14 27 5 | 42 44 38 43 44 37 41 41 33 44 39
8 | 9 10 14 13 13 5 12 8 10 20 4 | 23 29 25 24 24 22 28 26 29 30 24
9 | 7 11 14 12 13 4 12 7 8 24 4 | 34 36 34 36 33 32 37 35 36 40 34
10 | 11 14 13 10 13 7 11 8 13 15 4 | 37 39 36 38 31 34 39 34 38 38 35
11 | 8 11 16 9 17 5 12 11 12 30 4 | 33 39 26 36 44 29 32 37 37 41 33
12E | 10 16 10 7 17 5 23 8 15 10 5 | 51 50 44 48 46 45 45 46 48 47 46
13 | 14 14 15 13 19 6 14 11 14 14 5 | 38 36 31 41 43 33 35 37 40 30 35
14 | 12 16 13 10 15 7 12 6 11 15 4 | 36 35 32 43 37 34 35 33 40 32 35
15 | 10 20 9 14 16 6 17 9 9 18 5 | 38 40 31 40 36 30 34 33 38 32 35
16E | 17 14 8 10 16 8 20 8 10 12 5 | 58 47 43 49 46 45 47 47 51 41 48
17 | 9 15 16 12 15 8 19 15 10 30 5 | 30 35 28 31 34 27 30 40 35 31 31
18 | 10 12 8 12 19 5 14 11 8 18 4 | 36 35 35 31 34 32 35 30 32 37 32
19 | 13 12 14 13 19 5 15 13 13 24 5 | 35 39 31 40 39 32 35 39 43 31 36
20 | 12 12 10 12 16 4 12 11 11 21 4 | 39 37 39 39 34 36 40 34 38 38 36
21 | 11 9 14 8 18 8 12 10 11 25 4 | 29 28 26 26 29 24 26 26 28 25 25
22 | 8 12 9 10 18 7 8 8 6 19 3 | 29 31 28 27 33 28 29 24 30 32 26
23 | 24 17 13 15 16 4 16 11 11 26 6 | 43 39 33 44 39 33 34 37 38 34 36
24 | 8 7 14 7 16 4 16 9 9 11 4 | 36 39 37 37 36 33 38 35 35 31 36
25E | 13 13 18 9 22 11 19 20 15 18 6 | 142 140 139 140 140 141 76 146 144 145 141
26 | 11 11 10 15 10 6 14 9 10 24 4 | 30 29 29 34 30 27 29 30 30 35 30
X27 | 11 10 13 14 --- 8 15 9 15 13 5 | 32 31 26 29 --- 27 33 32 35 22 30
28E | 9 11 9 8 14 4 15 6 10 16 4 | 41 39 36 35 46 34 38 37 34 38 37
29 | 12 17 17 12 15 7 17 15 13 24 5 | 33 36 33 33 35 30 32 30 36 36 31
X30 | 4 --- --- --- --- 19 --- --- --- --- 0 | 47 --- --- --- --- 41 --- --- --- --- 47
31 | 15 16 15 10 22 7 12 22 15 25 6 | 30 41 27 36 40 28 37 31 36 32 31
32E | 20 14 13 12 18 7 12 20 15 13 6 | 146 144 141 140 140 142 140 146 144 139 142
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 13 13 11 16 6 15 12 12 22 |T 43 43 38 42 48 40 39 41 43 41 42
WRMS | 12 13 13 11 17 6 15 10 10 24 |NE 31 34 29 33 33 28 33 31 34 32 31
MEDI | 10 12 13 12 16 6 14 10 11 19 |MD 35 36 31 36 36 32 35 34 36 32 35
Table 3.1790.4 GPS week: 1790 Day: 4 MJD: 56778.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 8 14 12 13 5 14 10 11 13 4 | 28 33 26 31 35 26 36 31 33 21 29
2 | 8 9 13 12 10 4 13 10 9 30 4 | 18 24 21 24 18 17 22 23 22 20 19
3 | 6 9 13 11 14 4 8 8 7 48 3 | 23 27 22 23 26 22 26 26 29 51 22
4 | 5 10 10 13 11 5 10 10 8 18 3 | 25 26 22 29 26 22 25 27 30 24 24
5 | 8 22 9 16 17 5 19 11 17 21 5 | 25 31 19 27 27 21 28 22 34 24 23
X6E | 3 --- --- --- 576 103 --- --- --- --- 0 | 114 --- --- --- 172 46 --- --- --- --- 113
7 | 8 13 17 13 17 6 12 12 11 23 4 | 35 40 29 36 38 29 35 32 33 32 32
8 | 6 10 12 11 11 5 10 8 6 21 3 | 23 31 22 23 21 20 27 24 25 28 23
9 | 7 12 12 10 10 5 10 9 7 24 3 | 31 39 32 31 31 30 35 34 33 38 32
10 | 8 11 11 10 11 5 9 8 10 20 3 | 30 35 30 29 30 28 31 31 30 39 29
11 | 6 8 16 12 14 5 8 12 11 29 4 | 26 36 23 28 40 25 33 33 34 40 29
12E | 9 19 10 10 17 6 19 11 13 8 5 | 51 52 49 51 48 48 50 49 53 48 49
13 | 7 15 14 13 19 7 13 17 14 11 5 | 32 35 28 38 41 27 33 31 32 28 30
14 | 10 13 12 9 16 5 11 6 9 13 4 | 32 28 25 31 32 26 27 24 29 28 26
15 | 9 17 12 14 17 4 19 9 15 18 5 | 29 34 21 34 31 25 29 26 32 24 27
16E | 9 16 10 8 15 5 17 9 13 13 4 | 44 39 39 42 42 39 39 41 44 38 40
17 | 9 16 14 14 16 7 15 16 11 26 5 | 31 34 29 35 33 29 30 40 36 27 30
18 | 8 12 9 12 15 6 15 11 9 19 4 | 35 30 29 26 26 27 34 25 31 34 28
19 | 5 12 16 14 17 5 13 13 8 23 4 | 26 32 25 26 31 26 29 31 32 21 26
20 | 8 9 10 11 17 5 13 11 11 21 4 | 33 31 29 28 29 27 33 27 32 32 28
21 | 9 10 14 11 13 6 13 11 12 34 4 | 21 24 23 22 18 19 24 23 26 33 19
22 | 7 11 9 11 16 4 10 9 10 21 3 | 29 28 25 25 27 24 31 24 29 32 24
23 | 7 16 11 14 15 5 14 13 14 21 5 | 29 33 25 34 34 25 27 28 30 25 27
24 | 6 9 14 10 13 3 12 7 11 14 4 | 26 32 26 29 27 24 29 28 28 24 26
25E | 9 14 16 27 21 7 17 13 11 16 6 | 56 54 55 59 54 50 46 57 56 59 53
26 | 10 11 10 12 10 3 11 7 11 23 4 | 34 29 28 31 25 28 28 27 27 33 28
X27 | 13 9 15 12 --- 7 14 9 10 11 5 | 27 24 21 22 --- 20 28 26 25 17 23
28E | 7 11 10 10 11 5 12 8 8 11 3 | 44 45 42 44 49 42 43 49 49 42 44
29 | 10 16 14 13 15 4 19 13 14 24 5 | 28 31 28 28 27 24 30 29 30 28 24
X30 | 3 --- --- --- --- 15 --- --- --- --- 0 | 43 --- --- --- --- 36 --- --- --- --- 43
31 | 9 13 15 10 17 6 11 21 14 23 5 | 29 33 24 29 36 26 30 22 31 22 25
32 | 9 19 13 13 25 7 10 14 13 12 5 | 81 86 81 78 85 79 83 85 81 82 81
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 13 13 15 5 13 11 11 22 |T 35 35 29 33 38 29 33 32 34 33 33
WRMS | 8 13 13 12 14 5 13 10 10 20 |NE 27 30 24 27 28 23 29 26 29 29 25
MEDI | 8 12 12 12 15 5 13 10 11 21 |MD 29 32 26 29 31 26 30 28 31 28 28
Table 3.1790.5 GPS week: 1790 Day: 5 MJD: 56779.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 8 12 7 15 4 13 12 9 19 4 | 26 34 24 29 35 26 36 30 27 23 28
2 | 9 9 11 12 9 4 10 12 9 36 3 | 21 29 23 23 21 20 25 24 21 20 21
3 | 5 8 12 11 13 4 9 9 13 42 3 | 28 30 29 26 29 28 30 28 28 54 27
4 | 11 10 10 13 11 6 8 14 11 21 4 | 27 29 25 31 30 24 28 28 28 24 26
5 | 8 18 8 15 16 4 17 13 11 24 5 | 26 33 21 29 33 23 30 25 26 24 25
X6E | 4 --- --- --- 487 55 --- --- --- --- 0 | 44 --- --- --- 95 41 --- --- --- --- 44
7 | 7 12 16 16 14 5 11 10 12 26 4 | 32 39 30 37 36 30 34 31 29 33 31
8 | 4 9 12 10 9 5 10 9 10 17 3 | 23 30 23 24 25 23 27 25 21 28 23
9 | 6 11 13 9 9 6 9 10 10 16 3 | 37 41 36 37 35 36 38 38 35 39 36
10 | 7 10 11 13 10 4 9 10 12 19 3 | 33 36 33 31 34 32 38 32 37 41 33
11 | 10 10 15 11 16 7 10 13 13 28 4 | 27 37 24 30 41 26 35 33 28 43 29
12E | 12 17 7 11 20 4 19 14 9 12 5 | 40 39 32 39 37 34 33 39 38 36 36
13 | 8 15 11 16 18 6 12 17 14 12 5 | 30 34 25 33 38 25 30 29 29 23 27
14 | 9 12 10 9 14 5 12 8 8 20 4 | 31 29 24 30 30 26 27 25 30 25 27
15 | 10 21 8 13 16 4 15 15 11 16 5 | 31 40 24 34 35 26 29 29 30 24 28
16E | 9 18 8 8 14 4 17 14 13 13 5 | 49 45 44 46 46 45 45 43 47 42 44
17 | 10 13 13 18 16 5 14 17 12 32 5 | 27 34 26 32 30 25 27 38 27 27 27
18 | 8 13 9 12 16 4 12 14 9 19 4 | 33 32 28 29 36 26 31 26 28 26 28
19 | 7 14 14 15 17 5 12 14 9 25 4 | 25 34 25 29 32 25 29 30 27 24 26
20 | 12 11 9 10 16 5 11 16 10 22 4 | 33 31 28 30 32 28 31 28 31 28 28
21 | 9 8 13 12 14 6 11 13 12 34 4 | 20 26 24 23 25 19 26 22 23 33 20
22 | 6 10 11 12 17 5 8 11 9 19 4 | 23 26 24 21 31 22 25 22 24 21 22
23 | 9 17 11 20 15 4 14 13 11 23 5 | 28 34 24 34 32 25 27 27 30 22 26
24 | 7 8 12 11 16 4 12 6 14 16 4 | 30 34 31 32 31 28 32 30 30 27 29
25E | 8 11 15 13 20 7 14 19 10 15 5 | 97 101 100 101 99 98 59 101 98 100 98
26 | 10 9 9 12 9 5 9 8 11 19 3 | 32 34 28 33 27 27 29 29 23 32 28
X27 | 13 9 15 12 --- 7 12 11 13 9 5 | 27 25 24 22 --- 23 30 26 26 19 23
28E | 5 10 9 10 13 5 11 7 6 16 3 | 41 39 36 39 36 35 37 39 35 41 36
29 | 10 15 14 16 14 6 20 13 10 26 5 | 29 35 29 32 30 27 33 31 29 32 28
X30 | 4 --- --- --- --- 22 --- --- --- --- 0 | 40 --- --- --- --- 39 --- --- --- --- 41
31 | 9 12 13 9 15 5 12 24 7 25 5 | 30 35 23 27 35 25 30 26 27 27 25
32 | 9 13 11 11 19 6 10 17 10 13 4 | 56 59 57 56 52 58 56 58 54 58 55
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 12 13 15 5 12 13 11 23 |T 33 36 30 33 37 31 32 33 32 33 32
WRMS | 8 13 12 12 15 5 12 12 10 21 |NE 27 32 25 28 31 25 30 27 27 29 26
MEDI | 8 11 11 12 15 5 12 13 10 19 |MD 30 34 25 31 33 26 30 29 28 27 28
Table 3.1790.6 GPS week: 1790 Day: 6 MJD: 56780.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 8 13 10 15 4 13 13 11 13 4 | 34 43 32 40 44 35 44 40 38 28 37
2 | 11 8 10 12 12 4 10 12 9 32 4 | 18 27 22 24 25 20 25 26 19 21 20
3 | 8 8 12 12 14 4 8 9 13 48 4 | 37 38 33 33 40 35 35 35 34 56 35
4 | 10 7 10 10 15 4 9 13 8 23 3 | 22 29 23 27 34 22 25 29 23 28 24
5 | 10 13 8 16 19 4 15 16 11 21 5 | 25 28 17 26 35 19 28 21 25 19 22
X6E | 3 --- --- --- 484 67 --- --- --- --- 0 | 50 --- --- --- 101 64 --- --- --- --- 51
7 | 8 11 13 16 14 5 9 12 14 27 4 | 41 43 35 47 44 37 40 37 35 38 38
8 | 5 8 12 10 15 4 7 11 9 17 3 | 25 28 21 24 25 22 26 24 19 23 22
9 | 6 10 11 11 15 4 9 39 8 20 5 | 76 76 74 79 71 73 75 80 70 74 73
10 | 7 10 10 12 19 5 8 12 10 24 4 | 35 38 34 34 31 33 36 33 33 44 33
11 | 9 9 15 14 17 4 10 12 15 38 4 | 34 43 30 37 51 32 38 42 34 51 36
12E | 14 14 7 12 27 5 20 19 9 11 5 | 51 50 46 50 42 45 45 56 48 47 47
13 | 7 14 11 15 19 6 11 17 14 14 5 | 34 36 28 43 44 33 34 38 34 31 34
14 | 9 12 10 14 16 7 11 9 11 22 4 | 32 29 28 40 37 29 27 28 29 29 30
15 | 11 15 11 15 13 6 18 14 12 22 5 | 34 33 21 36 35 27 28 30 29 22 28
16E | 11 17 8 10 18 7 17 21 17 13 5 | 56 50 52 56 52 52 50 54 54 46 52
17 | 11 13 13 22 16 6 15 20 13 24 5 | 27 35 27 40 37 30 30 45 35 27 31
18 | 9 14 9 15 19 6 13 15 12 16 5 | 32 33 30 25 35 28 32 23 30 27 28
19 | 10 12 12 16 18 4 13 13 13 26 5 | 33 39 31 37 42 33 34 37 30 27 33
20 | 10 10 9 13 16 5 11 18 17 19 5 | 36 38 34 34 34 34 36 35 39 32 34
21 | 7 8 13 11 17 4 8 11 14 26 4 | 22 28 23 27 34 23 27 24 26 25 24
22 | 8 10 10 12 17 5 9 12 7 18 4 | 27 27 26 24 32 23 28 22 24 24 24
23 | 8 16 7 16 13 5 13 15 11 24 4 | 30 34 26 40 35 29 30 32 33 26 30
24 | 9 8 12 10 16 5 10 12 9 11 4 | 31 33 28 33 35 28 33 27 25 21 29
25E | 8 10 15 18 19 4 14 21 10 12 5 | 110 110 110 116 114 110 74 107 110 107 110
26 | 10 9 11 12 14 4 8 11 6 20 3 | 34 29 25 32 29 27 30 26 25 31 28
X27 | 12 9 13 15 --- 4 12 10 13 11 5 | 32 30 28 27 --- 27 31 31 24 21 28
28E | 7 10 9 9 15 3 13 16 9 33 4 | 56 59 55 54 60 56 58 63 57 65 57
29 | 13 13 15 14 17 7 15 17 10 23 5 | 35 35 32 32 40 29 33 29 30 32 31
X30 | 3 --- --- --- --- 14 --- --- --- --- 0 | 37 --- --- --- --- 34 --- --- --- --- 37
31 | 15 13 14 13 14 6 11 24 11 18 5 | 33 38 29 39 40 29 35 25 31 24 31
32 | 8 12 11 13 20 5 11 16 12 16 4 | 105 106 102 103 107 102 102 106 101 104 104
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 11 11 14 17 5 12 17 11 23 |T 40 42 36 41 46 38 38 40 38 38 38
WRMS | 9 11 11 13 16 5 11 14 10 22 |NE 31 33 27 32 35 28 32 30 29 30 29
MEDI | 9 10 11 13 16 5 11 13 11 20 |MD 34 35 29 36 37 30 33 32 31 28 31
Table 4: Precise Navigation Summary.
Weekly station RMS w.r.t. the estimated coordinates for the Latitude,
Longitude and Height components. See Table 5 for the daily summary.
CLK - Satellite clocks used.
EPO - Mean number of satellite clock epochs available in the daily
solutions.
Units: mm.
Table 4.1790 GPS week: 1790 MJD: 56774.0-56780.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3018 |U 6 7 14 |U 8 10 27 |U 7 9 15 |
emr | emr 2878 | 8 6 15 |U 8 11 26 | 8 12 20 |
esa | esa 2880 | 7 8 15 |U 8 11 28 |U 8 10 17 |
gfz | gfz 2877 |U 6 6 12 |U 8 11 27 |U 8 10 17 |
grg | grg 2880 |U 32 23 87 |U 9 11 28 |U 9 11 17 |
igr | igr 2880 | 6 7 13 | 8 11 25 | 8 10 16 |
igs | igs 2879 | 6 6 12 | 8 10 25 | 8 11 17 |
jpl | jpl 2850 | 7 7 16 |U 8 10 29 | 8 11 19 |
mit | mit 2880 | 6 6 13 |U 10 13 32 |U 11 14 22 |
Table 5: Daily Precise Navigation Summary using the corresponding Centre orbit
positions and satellite clock corrections at 15 min intervals.
Each line gives the daily station RMS w.r.t. the estimated coordinates
for the Latitude, Longitude and Height components.
CLK - Satellite clocks used.
EPO - Number of satellite clock epochs available for that day.
Units: mm.
Table 5.1790.0 GPS week: 1790 Day: 0 MJD: 56774.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3016 | 5 6 14 | 7 9 25 | 8 9 18 |
emr | emr 2876 | 7 5 14 | 9 9 24 | 8 9 22 |
esa | esa 2880 | 6 6 14 | 8 8 24 | 9 9 19 |
gfz | gfz 2872 | 5 5 12 | 8 10 30 | 8 9 18 |
grg | grg 2880 | 35 23 59 | 9 7 22 | 9 8 16 |
igr | igr 2880 | 6 5 12 | 8 7 22 | 9 8 17 |
igs | igs 2880 | 5 4 12 | 8 8 20 | 8 9 18 |
jpl | jpl 2876 | 6 4 13 | 9 8 28 | 8 10 22 |
mit | mit 2880 | 6 5 15 | 7 9 22 | 9 10 18 |
Table 5.1790.1 GPS week: 1790 Day: 1 MJD: 56775.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3022 | 7 5 11 | 6 9 25 | 7 11 14 |
emr | emr 2876 | 6 5 10 | 7 11 23 | 8 12 16 |
esa | esa 2880 | 6 6 11 | 6 10 28 | 9 11 15 |
gfz | gfz 2876 | 5 5 11 | 6 10 28 | 8 9 13 |
grg | grg 2880 | 6 7 17 | 7 10 27 | 9 11 16 |
igr | igr 2880 | 5 6 9 | 6 9 24 | 8 9 15 |
igs | igs 2879 | 5 4 9 | 6 9 24 | 8 10 14 |
jpl | jpl 2780 | 6 5 13 | 8 12 38 | 9 11 16 |
mit | mit 2880 | 5 4 9 | 9 17 42 | 9 12 14 |
Table 5.1790.2 GPS week: 1790 Day: 2 MJD: 56776.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3017 | 4 7 13 | 11 12 33 | 9 10 17 |
emr | emr 2876 | 8 9 15 | 8 12 31 | 9 12 25 |
esa | esa 2880 | 7 9 17 | 8 12 31 | 10 10 18 |
gfz | gfz 2876 | 6 8 12 | 9 12 25 | 10 12 20 |
grg | grg 2880 | 11 12 26 | 10 13 31 | 11 12 21 |
igr | igr 2880 | 6 8 12 | 9 13 31 | 10 11 18 |
igs | igs 2880 | 6 8 12 | 9 12 29 | 10 11 19 |
jpl | jpl 2780 | 10 11 17 | 7 8 24 | 10 10 20 |
mit | mit 2880 | 6 8 12 | 9 14 32 | 11 13 19 |
Table 5.1790.3 GPS week: 1790 Day: 3 MJD: 56777.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3024 | 5 4 12 | 7 10 36 | 7 9 16 |
emr | emr 2880 | 8 6 14 | 6 10 31 | 9 16 24 |
esa | esa 2880 | 6 8 15 | 6 8 35 | 8 11 18 |
gfz | gfz 2876 | 5 4 12 | 7 10 34 | 9 13 21 |
grg | grg 2880 | 31 30 125 | 6 11 32 | 9 12 21 |
igr | igr 2880 | 6 5 12 | 6 10 31 | 8 13 19 |
igs | igs 2880 | 6 5 12 | 6 9 32 | 8 13 20 |
jpl | jpl 2880 | 8 5 15 | 6 10 35 | 9 13 23 |
mit | mit 2880 | 5 4 13 | 9 11 34 | 9 14 19 |
Table 5.1790.4 GPS week: 1790 Day: 4 MJD: 56778.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3020 | 11 15 32 | 8 12 20 | 6 8 14 |
emr | emr 2880 | 11 12 23 | 9 9 22 | 8 11 21 |
esa | esa 2880 | 10 14 24 | 9 11 21 | 8 9 19 |
gfz | gfz 2880 | 11 10 21 | 8 12 19 | 7 10 18 |
grg | grg 2880 | 50 27 266 | 9 9 26 | 7 8 15 |
igr | igr 2880 | 12 11 22 | 9 11 17 | 7 8 16 |
igs | igs 2880 | 10 11 21 | 8 10 18 | 7 9 17 |
jpl | jpl 2880 | 11 13 24 | 10 11 23 | 8 11 23 |
mit | mit 2880 | 11 11 25 | 16 14 30 | 19 21 53 |
Table 5.1790.5 GPS week: 1790 Day: 5 MJD: 56779.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3008 | 5 5 8 | 11 15 28 | 7 10 16 |
emr | emr 2880 | 8 6 14 | 11 17 28 | 8 12 19 |
esa | esa 2880 | 6 8 14 | 12 17 34 | 7 9 16 |
gfz | gfz 2880 | 4 5 9 | 11 16 34 | 8 9 16 |
grg | grg 2880 | 46 27 69 | 12 15 34 | 9 11 18 |
igr | igr 2880 | 5 6 11 | 11 17 32 | 7 9 15 |
igs | igs 2880 | 5 5 10 | 11 17 30 | 8 10 16 |
jpl | jpl 2880 | 5 7 15 | 12 17 32 | 8 10 17 |
mit | mit 2880 | 4 4 10 | 11 20 33 | 8 12 17 |
Table 5.1790.6 GPS week: 1790 Day: 6 MJD: 56780.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3020 | 4 4 10 | 8 6 20 | 6 10 12 |
emr | emr 2880 | 7 4 13 | 8 8 20 | 7 13 16 |
esa | esa 2880 | 5 7 12 | 7 8 25 | 8 11 15 |
gfz | gfz 2880 | 4 4 9 | 7 8 22 | 7 11 14 |
grg | grg 2880 | 45 37 50 | 9 8 25 | 8 12 15 |
igr | igr 2880 | 5 5 10 | 7 8 21 | 7 10 14 |
igs | igs 2880 | 4 4 9 | 7 7 20 | 7 12 13 |
jpl | jpl 2878 | 6 5 13 | 7 7 21 | 8 13 16 |
mit | mit 2880 | 5 6 10 | 8 8 31 | 11 15 18 |
Table 6: Earth Orientation Parameters weekly summary.
Weekly mean and standard deviation of Centre ERP, ERP rates and
LOD differences with respect to IGS combined values. See Table 7 for
the daily summaries.
Xpole,Xrt: x pole and x pole rate
Ypole,Yrt: y pole and y pole rate
LOD : Length Of Day
AC LOD BIAS : 10-day mean LOD bias with respect to Bulletin A
AC LOD BIAS RMS: RMS of AC LOD BIAS
FLAG: "u" (used), "x" (excluded), "-" (no submission)
for Xpole, Ypole, Xrt, Yrt and LOD
Table 6.1790 GPS week: 1790 MJD: 56774.500-56780.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -25 -16 74 -10 -3 | 11 18
| 37 22 39 150 11 | 3
emr uuuuu | 55 -29 33 142 12 | 29 33
| 15 17 67 98 12 | 8
esa uuuuu | -2 1 21 10 -5 | 17 21
| 9 19 51 74 5 | 3
gfz uuuuu | -14 5 -81 -101 -2 | 16 19
| 21 16 85 140 5 | 3
grg uuuuu | 33 26 -273 118 -8 | 33 35
| 18 11 68 66 5 | 2
igr xxxxx | -6 29 11 -35 1 | -1 14
| 13 38 56 31 3 | 5
irf xxxxx | 10 -10 -7 -35 0 | -2 12
| 12 11 34 36 4 | 3
jpl uuuuu | 1 20 7 -37 8 | 17 24
| 29 19 95 96 14 | 5
mit uuuuu | -18 -51 30 -119 -3 | 22 25
| 46 40 84 94 6 | 3
ngs uuuuu | -4 56 93 36 0 | 5 10
| 54 84 120 157 6 | 4
sio xxxxx | 25 32 53 -69 -4 | 44 46
| 22 36 50 97 9 | 4
Table 7.1790.0 GPS week: 1790 Day: 0 MJD: 56774.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -5 -23 120 107 -3 | 10 15
emr uuuuu | 53 -48 78 46 0 | 25 28
esa uuuuu | 9 11 39 -7 -5 | 14 18
gfz uuuuu | -5 -11 -20 33 -9 | 14 18
grg uuuuu | 23 25 -310 175 -4 | 32 34
igr xxxxx | -17 58 -39 -15 0 | -5 15
irf xxxxx | -2 -18 11 -75 -4 | -4 11
jpl uuuuu | 21 14 -104 -44 -9 | 14 19
mit uuuuu | -72 -97 98 -217 -10 | 23 26
ngs uuuuu | -27 122 16 -130 5 | 2 7
sio xxxxx | 56 -21 4 -65 -16 | 48 50
Table 7.1790.1 GPS week: 1790 Day: 1 MJD: 56775.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 21 -45 37 144 1 | 10 15
emr uuuuu | 76 -52 48 -17 -7 | 24 28
esa uuuuu | 3 6 57 52 3 | 14 18
gfz uuuuu | 20 24 -212 120 2 | 13 17
grg uuuuu | 64 9 -335 158 -2 | 33 35
igr xxxxx | -10 84 102 -63 2 | -4 15
irf xxxxx | 15 -12 -5 -69 3 | -4 11
jpl uuuuu | 8 -6 -26 -103 7 | 13 19
mit uuuuu | -66 -103 86 -235 0 | 23 26
ngs uuuuu | -90 188 215 -117 -2 | 3 8
sio xxxxx | 27 -18 58 -155 -7 | 46 48
Table 7.1790.2 GPS week: 1790 Day: 2 MJD: 56776.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 15 -6 57 32 -23 | 12 16
emr uuuuu | 37 -6 42 159 24 | 23 27
esa uuuuu | 8 11 -35 152 -12 | 16 19
gfz uuuuu | -12 17 -87 -117 -6 | 15 18
grg uuuuu | 6 20 -175 124 -15 | 35 36
igr xxxxx | -5 37 5 -32 -2 | -2 14
irf xxxxx | 16 7 -55 9 -7 | -3 11
jpl uuuuu | -30 24 69 -190 -12 | 16 20
mit uuuuu | -17 -64 -104 -66 -12 | 22 25
ngs uuuuu | -9 35 215 -48 11 | 4 8
sio xxxxx | 43 40 -21 -38 -14 | 44 46
Table 7.1790.3 GPS week: 1790 Day: 3 MJD: 56777.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -49 18 96 90 -12 | 7 16
emr uuuuu | 43 -17 131 157 17 | 24 28
esa uuuuu | -5 25 58 11 -4 | 14 19
gfz uuuuu | -24 7 -129 -105 2 | 12 16
grg uuuuu | 43 34 -296 206 -6 | 30 32
igr xxxxx | -2 -9 -25 -10 2 | -4 15
irf xxxxx | -12 -3 -50 -48 2 | -6 12
jpl uuuuu | -43 2 135 -48 23 | 13 20
mit uuuuu | -46 7 -66 -156 -1 | 18 21
ngs uuuuu | 93 -64 16 -48 -1 | 3 8
sio xxxxx | -13 46 46 -181 -2 | 39 40
Table 7.1790.4 GPS week: 1790 Day: 4 MJD: 56778.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -42 2 42 -10 1 | 8 16
emr uuuuu | 46 -27 5 209 19 | 30 32
esa uuuuu | -12 -2 26 -22 -6 | 17 20
gfz uuuuu | -7 18 13 -284 -2 | 15 18
grg uuuuu | 32 41 -193 78 -12 | 31 33
igr xxxxx | -24 43 -6 -77 -2 | 0 11
irf xxxxx | 16 -3 18 -42 2 | -4 11
jpl uuuuu | 18 20 -25 -33 22 | 18 25
mit uuuuu | 1 -20 44 -106 1 | 19 22
ngs uuuuu | 2 -13 -8 172 -2 | 5 8
sio xxxxx | 18 65 84 -121 4 | 40 41
Table 7.1790.5 GPS week: 1790 Day: 5 MJD: 56779.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -81 -18 128 -196 8 | 12 21
emr uuuuu | 74 -38 6 275 20 | 36 41
esa uuuuu | -13 -34 65 -68 -2 | 20 24
gfz uuuuu | -25 -1 9 -231 -3 | 18 22
grg uuuuu | 32 18 -350 62 -7 | 33 35
igr xxxxx | -3 -21 76 -57 0 | 3 15
irf xxxxx | 18 -19 36 -40 3 | 0 15
jpl uuuuu | 40 44 -97 73 6 | 21 32
mit uuuuu | 47 -43 110 -88 2 | 22 26
ngs uuuuu | -6 77 -34 253 -5 | 9 14
sio xxxxx | 24 59 67 -31 8 | 43 46
Table 7.1790.6 GPS week: 1790 Day: 6 MJD: 56780.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -37 -37 40 -235 6 | 17 25
emr uuuuu | 55 -16 -83 163 13 | 43 48
esa uuuuu | -5 -7 -65 -48 -6 | 23 27
gfz uuuuu | -46 -19 -140 -126 4 | 21 26
grg uuuuu | 28 36 -250 22 -9 | 36 38
igr xxxxx | 17 8 -37 7 6 | 8 16
irf xxxxx | 18 -23 -4 17 -1 | 4 16
jpl uuuuu | -4 45 98 88 17 | 26 36
mit uuuuu | 27 -35 44 38 -2 | 25 30
ngs uuuuu | 6 46 228 171 -5 | 12 16
sio xxxxx | 21 55 130 107 -3 | 47 50
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